Kennedy Space Center Launch Complex 39

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Launch Complex 39
VAB Aerial - GPN-2000-000869.jpg
An aerial view of Launch Complex 39
Launch site Kennedy Space Center
Location 28°36′30.2″N 80°36′15.6″W / 28.608389°N 80.604333°W / 28.608389; -80.604333
Short name LC-39
Operator NASA
Total launches 151 (13 Saturn V, 4 Saturn IB, 135 Shuttle, 1 Ares I)
Launch pad(s) 2
Minimum / maximum
orbital inclination
28°–62°
Pad 39A launch history
Status Facility modifications underway for 2015 Falcon Heavy launch
Launches 92 (12 Saturn V, 80 Shuttle)
First launch November 9, 1967
Saturn V / Apollo 4
Last launch July 8, 2011
Space Shuttle Atlantis / STS-135
Associated rockets Saturn V (former)
Space Shuttle (former)
Falcon 9 v1.1 (future)
Falcon Heavy (future)
Pad 39B launch history
Status Facility modifications underway for 2017 SLS launch
Launches 59 (1 Saturn V, 4 Saturn IB, 53 Shuttle, 1 Ares I-X)
First launch May 18, 1969
Saturn V / Apollo 10
Last launch October 28, 2009
Ares I-X
Associated rockets Saturn V (former)
Saturn IB (former)
Space Shuttle (former)
Ares I-X (former)
Space Launch System (future)
Launch Complex 39
Location John F. Kennedy Space Center, Titusville, Florida
Area 7,000 acres (2,800 ha)
Built 1967
Governing body Federal
MPS John F. Kennedy Space Center MPS
NRHP Reference # 73000568[1]
Added to NRHP May 24, 1973
Launch Complex 39--Pad A
Location John F. Kennedy Space Center, Titusville, Florida
Area 160 acres (65 ha)
Built 1965
Governing body Federal
MPS John F. Kennedy Space Center MPS
NRHP Reference # 99001638[1]
Added to NRHP January 21, 2000
Launch Complex 39--Pad B
Location John F. Kennedy Space Center, Titusville, Florida
Area 160 acres (65 ha)
Built 1966
Governing body Federal
MPS John F. Kennedy Space Center MPS
NRHP Reference # 99001639[1]
Added to NRHP January 21, 2000

Launch Complex 39 (LC-39) is a rocket launch site at the John F. Kennedy Space Center on Merritt Island in Florida, USA. The site and its collection of facilities were originally built for the Apollo program, and was later modified for the Space Shuttle program, before currently undergoing modifications to support launches of the SpaceX Falcon 9 and Falcon Heavy and the Space Launch System.

Launch Complex 39 is composed of the two launch pads—39A and 39B—the Vehicle Assembly Building (VAB), the Crawlerway (the route used by crawler-transporters to carry Mobile Launcher Platforms between the VAB and the pads), the Orbiter Processing Facility buildings, the Launch Control Center (which contains the firing rooms), a news facility (famous for the iconic countdown clock seen in television coverage and photos), and various logistical and operational support buildings.[2]

SpaceX leases Launch Pad 39A from NASA and will be modifying the pad in 2014 to support Falcon Heavy launches as early as 2015.[3] NASA began modifying Launch Pad 39B in 2007 to accommodate the now defunct Project Constellation and is currently preparing Pad 39B for the Space Launch System[4][5] with first launch scheduled for 2017.

Launches from LC-39 have traditionally been supervised from the Launch Control Center (LCC), located 3 miles (4.8 km) from the launch pads, although it is unclear if SpaceX will use the LCC for their launches beginning in 2015. LC-39 is one of several launch sites that share radar and tracking services of the Eastern Test Range.

History[edit]

Early history[edit]

Northern Merritt Island was first developed 1890 when a few wealthy Harvard University graduates purchased 18,000 acres (73 km2) and constructed a three-story mahogany clubhouse, very nearly on the site of Pad 39A.[6] During the 1920s, Peter E. Studebaker Jr., son of the automobile magnate, built a small casino at De Soto Beach eight miles (13 km) north of the Canaveral lighthouse.[7]

In 1948, the Navy transferred the former Banana River Naval Air Station located south of Cape Canaveral, to the Air Force for use in testing captured German V-2 rockets.[8] The site's location on the East Florida coast was ideal for this purpose in that launches would be over the ocean, away from populated areas. This site became the Joint Long Range Proving Ground in 1949, and was renamed Patrick Air Force Base in 1950. The Air Force annexed part of Cape Canaveral to the North in 1951, forming the Air Force Missile Test Center, the future Cape Canaveral Air Force Station (CCAFS). Missile and rocketry testing and development would take place here through the 1950s.[9]

After the creation of NASA in 1958, the CCAFS launch pads were used for NASA's civilian unmanned and manned launches, including those of Project Mercury and Project Gemini.[10]

Apollo/Skylab/Apollo-Soyuz[edit]

Main article: Apollo program

In 1961, President Kennedy proposed to Congress the goal of landing a man on the Moon by the end of the decade. Congressional approval led to the launch of the Apollo program, which required a massive expansion of NASA operations, including an expansion of launch operations from the Cape to adjacent Merritt Island to the north and west.[11] NASA began acquisition of land in 1962, taking title to 131 square miles (340 km2) by outright purchase and negotiating with the state of Florida for an additional 87 square miles (230 km2). In July 1, 1962, the site was named the Launch Operations Center.[citation needed]

Initial design[edit]

Launch Complex Plan - 1963

At the time, the highest numbered launch pad on CCAFS was Launch Complex 37; when the lunar launch complex was designed, it was designated as Launch Complex 39. It was designed to handle launches of the Saturn V rocket, at the time the largest, most powerful rocket then designed, required to take Apollo to the Moon. Initial plans included five pads evenly spaced 8,700 feet (2,700 m) apart to avoid damage in the event of an explosion on the pad. Three were scheduled for construction (A-C, to the southeast) and two reserved for future use (D and E, west and north). The numbering of the pads at the time was from north to south, with the northernmost being 39A, and the southernmost being 39C. Pad 39A was never built, and 39C became 39A in 1963. With today's numbering, 39C would be north of 39B. Pad 39D would have been due west of 39C. Pad 39E would have been due north of the mid-distance between 39C and 39D, with 39E forming the top of a triangle, and equidistant from 39C and 39D. The Crawlerway was built with the additional pads in mind. This is the reason the Crawlerway turns as it heads to Pad B; continuing straight from that turn would have led to the additional pads.[12]

Integration of space vehicle stack[edit]

Apollo-Saturn 506 with Apollo 11 spacecraft being moved from the VAB to LC39A

Months before launch, the three stages of the Saturn V launch vehicle and the components of the Apollo spacecraft were brought inside the Vehicle Assembly Building (VAB) and assembled in one of four high bays into a 363-foot (111 m)-tall space vehicle on one of three Mobile Launchers. Each mobile launcher consisted of a two-story, 161-by-135-foot (49 by 41 m) launch platform with four hold-down arms and a 446-foot (136 m) Launch Umbilical Tower (LUT) topped by a crane used to lift the spacecraft into position for assembly. The MLP and unfueled vehicle together weighed 12,600,000 pounds (5,715 t).[13]

The Umbilical Tower contained two elevators and nine retractable swing arms which extended to the space vehicle, to provide access to each of the three rocket stages and the spacecraft for people, wiring and plumbing while the vehicle was on the launch pad, and swung away from the vehicle at launch.[13][14] Technicians, engineers, and astronauts used the uppermost Spacecraft Access Arm to access the crew cabin. At the end of the arm, the white room provided an environmentally controlled and protected area for astronauts and their equipment to enter the spacecraft.[citation needed]

Apollo era walkway and white room, on display at Kennedy Space Center Visitor Complex
Warning lamps showing the planned 3 pads including the unbuilt Pad C

Transportation to the pad[edit]

When the stack integration was completed, it was moved the 3–4 miles (4.8–6.4 km) to the pad at a speed of 1 mile (1.6 km) per hour by one of two Crawler-Transporters. Each crawler weighed 6,000,000 pounds (2,720 t) and was capable of keeping the space vehicle on its Mobile Launcher level while negotiating a 5 percent grade to the pad. At the pad, the MLP was supported by six steel pedestals, plus four additional extensible columns.[13]

Mobile Service Structure[edit]

Saturn V with fixed (left) and mobile (right) service structures

After the MLP was set in place, the Crawler-Transporter rolled a 410-foot (125 m), 10,490,000-pound (4,760 t) Mobile Service Structure (MSS) into place to provide further access for technicians to perform detailed checkout of the vehicle, and necessary umbillical connections to the pad. The MSS contained three elevators, two self-propelled platforms and three fixed platforms, and was rolled back 6,900 feet (2,100 m) to its parking position shortly before launch.[13]

Flame deflector[edit]

A flame deflector was slid on rails into place under the launch pedestal. This system allowed for rotation with a second flame deflector, after the first was refurbished after each launch. Each deflector measured 39 feet (12 m) high by 49 feet (15 m) wide by 75 feet (23 m) long and weighed 1,400,000 pounds (635 t). It deflected the exhaust flame into a trench measuring 43 feet (13 m) deep by 59 feet (18 m) wide by 449 feet (137 m) long.[13]

Launch control and fueling[edit]

The four-story Launch Control Center was located 3.5 miles (5.6 km) away from Pad A, adjacent to the Vehicle Assembly Building for safety. The third floor had four firing rooms (corresponding to the four high bays in the VAB), each with 470 sets of control and monitoring equipment.[when?] The second floor contained telemetry, tracking, instrumentation, and data reduction computing equipment. The LCC was connected to the Mobile Launchers by a high speed data link, and during launch a system of 62 closed-circuit television cameras transmitted to 100 monitor screens in the LCC.[13]

Large cryogenic tanks located near the pads stored the liquid hydrogen and liquid oxygen (LOX) for the second and third stages of the Saturn V. The highly explosive nature of these chemicals required numerous safety measures at the Launch Complex. The pads were located 8,730 feet (2,660 m) away from each other.[13] Before tanking operations began and during launch, non-essential personnel were excluded from the danger area.

Emergency evacuation system[edit]

Each pad had a 200-foot (61 m) evacuation tube running from the Mobile Launcher platform to a blast-resistant bunker 39 feet (12 m) underground, equipped with survival supplies for 20 persons for 24 hours. There was also a cab/slidewire system running from the 322-foot (98 m) tower level to evacuate astronauts and technicians 2,503 feet (763 m) away from the pad.[citation needed]

Pad Terminal Connection Room[edit]

LC39A Pad Terminal Connection Room, 2nd floor hallway

Connections between the Launch Control Center, mobile launcher platform and space vehicle are made in the Pad Terminal Connection Room (PTCR). The facility was a two-story series of rooms beneath the launch pad, constructed of reinforced concrete located on the west side of the flame trench and was protected by up to 20 feet (6.1 m) of fill dirt.[15][16]

Sound suppression water system[edit]

SSWS pipes beneath LC39A

An elevated water tank near each pad provided sound buffering protection for the launching spacecraft. Part of the Sound Suppression Water System (SSWS), the 290-foot (88 m) water towers stored 300,000 gallons (1.1 Megalitres) of water, which was released just before engine ignition.[17] The water discharged onto the launch platform during lift-off muffled the intense sound waves produced by the first stage Rocketdyne F-1 engines. Due to heating of the water, a large quantity of steam was produced during launch.

Apollo and Skylab launches[edit]

The first flight of the Saturn V (on the unmanned Apollo 4 flight) rising from Pad 39A

The first use of LC-39 came in 1967 with the first Saturn V launch, carrying the unmanned Apollo 4 spacecraft. The second unmanned launch, Apollo 6, also used Pad 39A. With the exception of Apollo 10, which used Pad 39B (due to the "all-up" testing resulting in a 2-month turnaround period), all manned Apollo-Saturn V launches, commencing with Apollo 8, used Pad 39A.

A total of thirteen Saturn Vs were launched for Apollo, and the unmanned launch of the Skylab space station in 1973. The mobile launchers were then modified for the shorter Saturn IB rockets, by adding a "milk-stool" extension platform to the launch pedestal, so that the S-IVB upper stage and Apollo spacecraft swing arms would reach. These were used for three manned Skylab and one Apollo-Soyuz flights, since the Saturn IB pads 34 and 37 at Cape Canaveral AFB had been decommissioned.[citation needed]

Space Shuttle[edit]

Launch of the final Saturn IB rocket from Pad 39B on July 15, 1975 carrying the Apollo-Soyuz Test Project Command Module into orbit
Enterprise on Pad 39A during the fit check tests in 1979
Columbia in launch configuration at Pad 39A in preparation for STS-1

The thrust to allow the Space Shuttle to achieve orbit was provided by a combination of the Solid Rocket Boosters (SRBs) and the Space Shuttle Main Engines (SSMEs). The SRBs used solid propellant, hence their name. The SSMEs used a combination of liquid hydrogen and liquid oxygen (LOX) from the External Tank (ET), as the orbiter did not have internal fuel tanks for the SSMEs (as they would be have had to be as large as the External Tank). The SRBs arrived in segments via rail car from their manufacturing facility in Utah, the External Tank arrived from its manufacturing facility in Louisiana by barge, and the orbiter waited in the Orbiter Processing Facility (OPF). The SRBs were first stacked in the VAB, and then the External Tank was mounted between them. Then, using a massive crane, the orbiter was lowered and connected to the External Tank.

Payload to be installed at the launch pad was independently transported in a payload transportation canister then installed vertically at the Payload Changeout Room. Otherwise, payloads would have already been pre-installed at the Orbiter Processing Facility and transported within the orbiter's cargo bay.

The original structure of the pads was remodeled for the needs of the Space Shuttle, starting with Pad 39A after the last Saturn V launch, and in 1977 for Pad 39B after the Apollo-Soyuz Test Project in 1975.

Launch towers[edit]

Each pad contained a two-piece access tower system, the Fixed Service Structure (FSS) and the Rotating Service Structure (RSS). The FSS permitted access to the Shuttle via a retractable arm and a "beanie cap" to capture vented LOX from the External Tank. The RSS contained the Payload Changeout Room, which offered "clean" access to the orbiter's payload bay, protection from the elements, and protection in winds up to 60 knots (110 km/h).

Space Shuttle launches[edit]

After the launch of Skylab in 1973, Pad 39A was reconfigured for the Space Shuttle and was used for the first Shuttle launch (STS-1), using the Columbia in 1981.[18] After Apollo 10, Pad 39B was kept as a backup launch facility in the case of the destruction of 39A, but saw service for all three Skylab missions, the ASTP flight, as well as un-launched Skylab Rescue flight. After ASTP, 39B underwent the same reconfiguration as 39A, but due to necessary modifications (mainly to allow the facility to service a modified Centaur-G upper stage), along with budgetary restraints, it was not ready until 1986, and the first Shuttle launch to use it was the ill-fated STS-51-L flight – the Challenger disaster But the first successful Shuttle launch to use 39B was STS-26 – The 1988 Return to Flight since the Challenger Disaster.

For the Shuttle, the pad had a fixed tower (left over from the Apollo-Saturn era) and a rotating service platform, used to protect the Shuttle Orbiter and to install vertically handled payloads into the payload bay.[4][19]

Swing arm modifications[edit]

The doors to the White Room, which provided entry to the Shuttle crew compartment, are seen here at the end of the access arm walkway

The Gaseous Oxygen Vent Arm positioned a hood, often called the "Beanie Cap," over the top of the External Tank (ET) nose cone during fueling.[when?] Heated gaseous nitrogen was used there to remove the extremely cold gaseous oxygen that normally vented out of the External Tank. This prevented the formation of ice that could fall and damage the shuttle.[citation needed]

The Hydrogen Vent Line Access Arm mated the External Tank (ET) Ground Umbilical Carrier Plate (GUCP) to the launch pad hydrogen vent line. The GUCP provided support for plumbing and cables, called umbilicals, that transferred fluids, gases, and electrical signals between two pieces of equipment. While the ET was being fueled, hazardous gas was vented from an internal hydrogen tank through the GUCP, out a vent line to a flare stack where it was burned off at a safe distance. Sensors at the GUCP measured gas level. The GUCP was redesigned after leaks created scrubs of STS-127 and were also detected during attempts to launch STS-119 and STS-133.[20] The GUCP released from the ET at launch and fell away with a curtain of water sprayed across it for protection from flames.

Emergency pad evacuation[edit]

M113 armored personnel carriers parked near LC-39

In an emergency, the launch complex used a slidewire escape basket system for quick evacuation. Assisted by members of the closeout team, the crew would leave the orbiter and ride an emergency basket to the ground at speeds reaching up to 55 miles per hour (89 km/h).[21] From there, the crew took shelter in a bunker. A modified M113 Armored Personnel Carrier could carry injured astronauts away from the complex to safety.[22]

During the launch of Discovery on STS-124 on May 31, 2008, the pad at LC-39A suffered extensive damage, in particular to the concrete trench used to deflect the SRB's flames.[23] The subsequent mishap investigation found that the damage was the result of carbonation of epoxy and corrosion of steel anchors which held the refractory bricks in the trench in place. These had been exacerbated by the fact that hydrochloric acid is an exhaust by-product of the solid rocket boosters.[24]

Project Constellation and Pad 39B[edit]

Ares I-X launches from LC-39B, 15:30 UTC, October 28, 2009
Pad 39B undergoing construction for Ares

Former NASA plans[when?] for Project Constellation called for the reverting of both pads to a state similar to that of the Apollo Program, but with the installation of lightning masts to deflect lightning strikes away from the Ares I and Ares V rockets.[citation needed] However, the only modifications made for Constellation were to Pad 39B.

The last Shuttle launch from Pad 39B was the nighttime launch of STS-116 on December 9, 2006. To support the final Shuttle mission STS-125 launched from Pad 39A in May 2009, Endeavour was placed on 39B if needed to launch the STS-400 rescue mission. Modifications were made to 39B in the mean time, including installation of three new 600 ft.-tall lightning mast towers similar to those used on the Atlas V and Delta IV launch pads at nearby Cape Canaveral, and removal of the existing single lightning mast and a crane assembly which dated back to the Apollo program.[citation needed]

After the completion of STS-125, 39B was converted[how?] for the single test flight of the Project Constellation Ares I-X from Pad 39B on October 28, 2009.[citation needed]

2011–2013[edit]

With the retirement of the Shuttle in 2011,[25] and the cancellation of Project Constellation in 2010, the future of LC-39 entered a time where the future use of the pads was uncertain. By early 2011, NASA began informal discussions on use of the pads and facilities by private companies to fly missions for the commercial space market.[26][dated info]

Pad 39A[edit]

Just like the first 24 shuttle flights, Pad 39A supported the final manifested shuttle flights, starting with STS-117 in June 2007 until the retirement of the shuttle fleet in July 2011. As of late 2013, the pad remained as it was when Atlantis launched on the final shuttle mission on July 8, 2011, complete with a mobile launcher platform.[citation needed]

Bob Cabana, director of KSC, announces the signing of the Pad 39A lease agreement on 14 April 2014

By early 2013, NASA publicly announced that they would allow commercial launch providers to lease Pad 39A,[27] and followed that, in May 2013, with a formal solicitation for proposals for commercial use of Launch Pad 39A.[28] There were two competing bids for the commercial use of the launch complex.[29] SpaceX submitted a bid for exclusive use of the launch complex, while Jeff Bezos' Blue Origin submitted a bid for shared non-exclusive use of the complex such that the launchpad would interface with multiple vehicles, and costs could be shared over the long term. One potential shared user in the Blue Origin plan was United Launch Alliance.[30] Prior to completion of the bid period, and prior to any public announcement by NASA of the results of the process, Blue Origin filed a protest with the U.S. General Accounting Office (GAO) "over what it says is a plan by NASA to award an exclusive commercial lease to SpaceX for use of mothballed space shuttle launch pad 39A."[31] NASA had planned to complete the bid award and have the pad transferred by October 1, 2013, but the protest "will delay any decision until the GAO reaches a decision, expected by mid-December."[31] On 12 December 2013, the GAO denied the protest and sided with NASA, which argued that the solicitation contains no preference on the use of the facility as multi-use or single-use. "The [solicitation] document merely asks bidders to explain their reasons for selecting one approach instead of the other and how they would manage the facility."[32]

On December 13th, 2013, NASA announced that they had selected SpaceX as the new commercial tenant.[33] SpaceX signed the lease agreement on 14 April 2014.[34] They have been given a twenty year exclusive lease of Pad 39A.[29] SpaceX plans to launch their Falcon 9 and Falcon Heavy from the pad and build a new hangar near it.[35][29][34] Elon Musk, CEO of SpaceX, has stated that he wants to shift most of their NASA launches to Pad 39A, including Commercial Cargo and Crew missions to the International Space Station.[33][36]

Current status[edit]

The aerial view of both launch pads at the complex, 39A (foreground) and 39B

As of 2014, Launch Complex 39 is in the midst of substantial modification to prepare for new uses with new vehicles. SpaceX has leased Launch Pad 39A for use with Falcon 9, Falcon Heavy (2015), and possibly other SpaceX launchers, while Launch Pad 39B, the Vehicle Assembly Building and Crawlerway are being readied for launches of the government-owned Space Launch System[37] beginning in 2017.

Launch Pad 39A[edit]

SpaceX signed a 20-year lease for Launch Pad 39A on 14 April 2014. The pad is currently being modified to support launches of both Falcon 9 v1.1 and Falcon Heavy launch vehicles, which will include the construction of a horizontal integration facility, similar to that used at existing SpaceX-leased facilities at Cape Canaveral Air Force Station and Vandenberg Air Force Base – this is a marked difference from the vertical integration process used by NASA's own Apollo and Space Shuttle vehicles at the Launch Complex 39. Additionally new instrumentation and control systems will be installed and substantial new plumbing will be added for a variety of rocket liquids and gasses.[3]

SpaceX has indicated they may be ready to accomplish the first launch at pad 39A—a Falcon Heavy—as early as 2015,[3] as they have had architects and engineers working on the new design and modifications since 2013.[37][38]

SpaceX intends to utilize the Fixed Service Structure (FSS) of the Pad 39A launch towers, and will extend it above its existing 350 feet (110 m)-height, but will not need the Rotating Service Structure (RSS) and may remove it. They will also construct a new launch crown over the existing infrastructure.[38] NASA has already removed the Orbiter Servicing Arm and white room by which astronauts entered the Space Shuttle.[38] Launch vehicles will be assembled horizontally in a hangar near the pad, transferred to the pad, and then lifted atop a launch platform for the remainder of the launch prep and lift off.[37]

For military missions from Pad 39A, payloads will be vertically integrated, as that is required per launch contract with the US Air Force.[37]

Pad 39A will be used to host launches of astronauts on the crewed-version of the Dragon space capsule in a public–private partnership with NASA. The NASA plan as of April 2014 calls for the first NASA crewed missions in 2017.[37]

Launch Pad 39B[edit]

Since the Ares I-X flight, NASA proceeded with plans to strip Pad 39B of its Flight Service Structure (FSS), returning the location to an Apollo-like "clean pad" design for the first time since 1977. This approach will make the pad available to multiple types of vehicles which arrive at the pad with service structures on the mobile launcher platform as opposed to custom structures on the pad.[39] The LH2, LOX, and water tanks (used for the sound suppression system) are the only structures left from the Shuttle era.[40][41]

As of April 2014, NASA has one SLS mission scheduled in 2017, and a second one in 2021.[37]

As of June 2012, repairs and modifications to selected facility systems at Launch Complex (LC) 39B for Space Launch System (SLS) processing and launch operations are finishing the first phase of a five-phase project. The second phase of this project is currently budgeted at $89.2 million ($6.1 million in FY 2012, $28.5 million in FY 2013, $9.4 million in FY 2014 and $45.2 million in the outyears).[42][dated info]

In 2014, NASA announced that it would make Pad 39B available to commercial users during times when it is not needed by the Space Launch System.[37]

See also[edit]


References[edit]

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  2. ^ "KSC Facilities". NASA. Retrieved 2009-07-06. 
  3. ^ a b c Dean, James (2014-04-14). "With nod to history, SpaceX gets launch pad 39A OK". Florida Today. Retrieved 2014-04-15. 
  4. ^ a b NASA (1993). "Launch Complex 39-A & 39-B". National Aeronautics and Space Administration. Retrieved September 30, 2007. 
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  16. ^ Young, John; Robert Crippen. Get this book in print▼ My library My History eBookstore Wings in Orbit: Scientific and Engineering Legacies of the Space Shuttle 1971-2010 (Hardcover): Scientific and Engineering Legacies of the Space Shuttle 1971-2010. p. 82. ISBN 978-0-16-086847-4. 
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  21. ^ "SPACE.com – NASA Conducts Shuttle Astronaut Rescue Drill". Retrieved 2007-10-22. 
  22. ^ "NASA Field Journal by Greg Lohning". Retrieved 2008-11-01. 
  23. ^ SPACE.com -- NASA Eyes Launch Pad Damage for Next Shuttle Flight
  24. ^ Lilley, Steve K. (August 2010). "Hit the Bricks". System Failure Case Studies (NASA) 4 (8): 1–4. Retrieved July 20, 2011. 
  25. ^ NASA: Lost in Space, Business Week, 2010-10-28, accessed 2010-10-31.
  26. ^ Dean, James (2011-02-06 quote=As the shuttle program nears retirement, KSC officials are evaluating whether other facilities that supported three decades of shuttle flights will transition to serve new vehicles or be discarded. The center is offering use of its launch pads, runway, Vehicle Assembly Building high bays, hangars and firing rooms to private companies expected to play a bigger role in NASA missions and a growing commercial space market.). "Up for grabs? Private companies eye KSC facilities". Florida Today. Retrieved 2011-02-06. 
  27. ^ "NASA not abandoning LC-39A" January 17, 2013, accessed February 7, 2013.
  28. ^ NASA requests proposals for commercial use of Pad 39A, NewSpace Watch, 20 May 2013, accessed 21 May 2013.
  29. ^ a b c "Selection Statement for Lease of Launch Complex 39A". NASA. 12 December 2013. Retrieved 23 December 2013. 
  30. ^ Matthews, Mark K. (2013-08-18). "Musk, Bezos fight to win lease of iconic NASA launchpad". Orlando Sentinel. Retrieved 2013-08-21. 
  31. ^ a b Messier, Doug (2013-09-10). "Blue Origin Files Protest Over Lease on Pad 39A". Parabolic Arc. Retrieved 2013-09-11. 
  32. ^ Messier, Doug (2013-12-12). "Blue Origin Loses GAO Appeal Over Pad 39A Bid Process". Parabolic Arc. Retrieved 2013-12-13. 
  33. ^ a b Clark, Stephen (13 December 2013). "SpaceX to begin negotiations for shuttle launch pad". SpaceflightNow. Retrieved 13 December 2013. 
  34. ^ a b Dean, James (14 April 2014). "SpaceX takes over KSC pad 39A". Florida Today. Retrieved 15 April 2014. 
  35. ^ Gwynne Shotwell (2014-03-21). Broadcast 2212: Special Edition, interview with Gwynne Shotwell (mp3) (audio file) (in English). The Space Show. Event occurs at 20:00–21:10. 2212. Archived from the original on 2014-03-22. Retrieved 2014-03-22. 
  36. ^ Clark, Stephen (12 December 2013). "GAO decision opens door for commercial lease of pad 39A". Spaceflight Now. Retrieved 23 December 2013. "Musk said he wants to launch SpaceX's commercial cargo and crew missions to the International Space Station from launch pad 39A" 
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  38. ^ a b c "NASA signs over historic Launch Pad 39A to SpaceX". collectSpace. 2014-04-14. Retrieved 2014-04-15. 
  39. ^ "Historic space shuttle pad soon to be scrap". USA Today. 23 March 2011. 
  40. ^ NASA (2006). "Sound Suppression System". NASA. Retrieved September 30, 2007. 
  41. ^ "STS-127 Rollaround starts". Space Flight Now. 
  42. ^ http://www.nasa.gov/pdf/632670main_NASA_FY13_Budget_CECR-508.pdf NASA FY13 Budget

External links[edit]


Coordinates: 28°36′30″N 80°36′16″W / 28.608397°N 80.604345°W / 28.608397; -80.604345